GB8706686D0 - Thrust deflectors - Google Patents

Thrust deflectors

Info

Publication number
GB8706686D0
GB8706686D0 GB878706686A GB8706686A GB8706686D0 GB 8706686 D0 GB8706686 D0 GB 8706686D0 GB 878706686 A GB878706686 A GB 878706686A GB 8706686 A GB8706686 A GB 8706686A GB 8706686 D0 GB8706686 D0 GB 8706686D0
Authority
GB
United Kingdom
Prior art keywords
thrust deflectors
deflectors
thrust
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB878706686A
Other versions
GB2188886B (en
GB2188886A (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of GB8706686D0 publication Critical patent/GB8706686D0/en
Publication of GB2188886A publication Critical patent/GB2188886A/en
Application granted granted Critical
Publication of GB2188886B publication Critical patent/GB2188886B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/423—Braking devices acting by reaction of gaseous medium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/563—Reversing jet main flow in specified direction, e.g. to obviate its reinjection
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
GB8706686A 1986-04-14 1987-03-20 Thrust deflectors for turbomachine propulsion nozzles Expired - Fee Related GB2188886B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/851,931 US4805840A (en) 1986-04-14 1986-04-14 Thrust deflectors for propulsion nozzles of turbomachines

Publications (3)

Publication Number Publication Date
GB8706686D0 true GB8706686D0 (en) 1987-04-23
GB2188886A GB2188886A (en) 1987-10-14
GB2188886B GB2188886B (en) 1990-01-31

Family

ID=25312084

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8706686A Expired - Fee Related GB2188886B (en) 1986-04-14 1987-03-20 Thrust deflectors for turbomachine propulsion nozzles

Country Status (2)

Country Link
US (1) US4805840A (en)
GB (1) GB2188886B (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2727468B1 (en) * 1994-11-30 1996-12-27 Hispano Suiza Sa DOWNSTREAM OBSTACLE TURBOREACTOR DRIVER
US20060150612A1 (en) * 2005-01-12 2006-07-13 Honeywell International Inc. Thrust vector control
FR2946741B1 (en) * 2009-06-12 2015-09-18 Mbda France SYSTEM FOR CONTROLLING THE TRACK OF A MU MOBILE BY REACTION.
FR2967766B1 (en) * 2010-11-24 2012-12-28 Mbda France SYSTEM FOR DRIVING AROUND ROTATION AXES A REACTION MOBILE MOBILE, IN PARTICULAR A MISSILE
US10040563B1 (en) * 2013-04-11 2018-08-07 Geoffrey P. Pinto Dual panel actuator system for jet engines
CN106968831A (en) * 2016-01-14 2017-07-21 王佐良 A kind of rudder formula vector engine
FR3060660B1 (en) * 2016-12-20 2019-05-17 Safran Nacelles AIRCRAFT TURBO BURNER BOAT, PROPULSIVE AND AIRCRAFT ASSEMBLY COMPRISING SUCH A NACELLE
US11994087B2 (en) 2021-12-06 2024-05-28 Rohr, Inc. Variable area nozzle and method for operating same
US11867136B2 (en) 2021-12-17 2024-01-09 Rohr, Inc. Variable area nozzle assembly and method for operating same
US11754018B2 (en) 2021-12-17 2023-09-12 Rohr, Inc. Aircraft propulsion system exhaust nozzle with ejector passage(s)
US11867135B1 (en) 2022-09-14 2024-01-09 Rtx Corporation Vectoring exhaust nozzle for an aircraft powerplant

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB688011A (en) * 1950-06-28 1953-02-25 Armin Wenger Control arrangement for jet-propulsion
FR1115172A (en) * 1954-11-29 1956-04-20 Snecma Improvements to jet diverter devices, particularly intended for nozzles or thrusters
GB850012A (en) * 1956-08-23 1960-09-28 Power Jets Res & Dev Ltd Improvements relating to the deflection of fluid jets
US3401886A (en) * 1966-05-12 1968-09-17 Lockheed Aircraft Corp Thrust vector control device
GB1327385A (en) * 1969-12-09 1973-08-22 Secr Defence Jet propulsion apparatus aircraft
GB1381397A (en) * 1971-02-26 1975-01-22 Mtu Muenchen Gmbh Jet pipe arrangement for a jet-propulsion engine
DE2248480C3 (en) * 1972-10-03 1975-10-09 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Turbine jet engine for aircraft taking off or landing vertically or briefly

Also Published As

Publication number Publication date
US4805840A (en) 1989-02-21
GB2188886B (en) 1990-01-31
GB2188886A (en) 1987-10-14

Similar Documents

Publication Publication Date Title
EP0260036A3 (en) Cyrostat assembly
GB8609228D0 (en) Thrusters
GB2200412B (en) Thrust bearing
GB2196911B (en) Thrust reverser
ZA855085B (en) Thrust unit
GB8702659D0 (en) Thrust bearings
GB8725983D0 (en) Thrust bearing
GB8629448D0 (en) Extractor
GB8706686D0 (en) Thrust deflectors
GB8626129D0 (en) Pile-framed structure
GB2169970B (en) Thrust washer
GB8724088D0 (en) Cutter-bit assemblies
GB8629322D0 (en) Cyano-terpenoid esters
GB8707535D0 (en) Operating multiple-electromagnet arrangement
AP8700067A0 (en) Fluorebenzyl esters
GB2196067B (en) Thrust bearing assembly
GB2198208B (en) Gland
GB8621726D0 (en) Sunroof assembly
GB8610670D0 (en) Enzyme
GB8709988D0 (en) Gear-lever assembly
GB8714139D0 (en) Feeder-burner assembly
GB8613430D0 (en) Enzyme
GB8727141D0 (en) Micromanipulator
ZA873008B (en) Thrust principle
GB8623372D0 (en) Material-separating assemblies

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19990320